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dc.contributor.advisorChang, Liang-Wey
dc.contributor.authorLaufenberg, Robert S.
dc.dateMarch 1987
dc.date.accessioned2012-11-27T00:28:12Z
dc.date.available2012-11-27T00:28:12Z
dc.date.issued1987-03
dc.identifier.urihttp://hdl.handle.net/10945/22692
dc.description.abstractThe requirement to develop a space based remote ocean sensing platform exists within the Department of the Navy. This project models a satellite subsystem with structural flexibility utilizing the Equivalent Rigid Link System (ERLS) . Dynamic analysis with computer simulation is presented for a simple flexible boom rotating in three dimensions with and without a point mass at the boom tip.
dc.description.urihttp://archive.org/details/computersimulati1094522692
dc.format.extent90 p.en_US
dc.language.isoen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
dc.subject.lcshMechanical engineeringen_US
dc.titleComputer simulation of a rotational single-element flexible spacecraft boom.en_US
dc.typeThesisen_US
dc.contributor.secondreaderShin, Young S.
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentMechanical Engineering
dc.subject.authorflexible manipulatoren_US
dc.subject.authorspacecraften_US
dc.description.serviceLieutenant, United States Navy
etd.thesisdegree.nameM.S. in Mechanical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineMechanical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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